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GOE 758 AIRFOIL (goe758-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 758 AIRFOIL (goe758-il)
Reynolds number: 1,000,000
Max Cl/Cd: 133.59 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe758-il-1000000.txt
Download as CSV file: xf-goe758-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 758 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.1069   0.08443   0.08254  -0.0798   0.9014   0.0224
 -10.750  -0.1025   0.08098   0.07899  -0.0812   0.8801   0.0233
 -10.500  -0.1232   0.07143   0.06940  -0.0859   0.8703   0.0251
 -10.250  -0.1329   0.06501   0.06292  -0.0883   0.8581   0.0251
 -10.000  -0.1544   0.05735   0.05524  -0.0905   0.8467   0.0255
  -9.750  -0.2874   0.03092   0.02856  -0.1106   0.8416   0.0256
  -9.500  -0.2996   0.02904   0.02659  -0.1096   0.8269   0.0257
  -9.250  -0.3128   0.02678   0.02419  -0.1078   0.8127   0.0258
  -9.000  -0.3139   0.02458   0.02187  -0.1068   0.7985   0.0259
  -8.750  -0.3048   0.02323   0.02043  -0.1059   0.7821   0.0261
  -8.500  -0.3000   0.02127   0.01830  -0.1049   0.7631   0.0263
  -8.250  -0.2900   0.01976   0.01664  -0.1040   0.7389   0.0267
  -8.000  -0.2813   0.01791   0.01455  -0.1030   0.7117   0.0271
  -7.750  -0.2699   0.01628   0.01267  -0.1019   0.6870   0.0279
  -7.500  -0.2528   0.01658   0.01248  -0.1002   0.6690   0.0299
  -7.250  -0.2536   0.01175   0.00711  -0.0988   0.6595   0.0305
  -7.000  -0.2351   0.01013   0.00538  -0.0984   0.6503   0.0310
  -6.750  -0.2130   0.00924   0.00444  -0.0981   0.6432   0.0314
  -6.500  -0.1909   0.02020   0.01505  -0.1022   0.6448   0.0319
  -6.250  -0.1721   0.01748   0.01187  -0.1005   0.6382   0.0281
  -6.000  -0.1482   0.01662   0.01084  -0.0998   0.6323   0.0284
  -5.750  -0.1237   0.01575   0.00983  -0.0993   0.6270   0.0285
  -5.500  -0.0991   0.01493   0.00886  -0.0987   0.6218   0.0284
  -5.250  -0.0738   0.01423   0.00805  -0.0982   0.6173   0.0284
  -5.000  -0.0479   0.01357   0.00732  -0.0978   0.6132   0.0285
  -4.750  -0.0221   0.01301   0.00668  -0.0974   0.6090   0.0285
  -4.500   0.0037   0.01254   0.00613  -0.0969   0.6047   0.0287
  -4.250   0.0298   0.01211   0.00565  -0.0965   0.6007   0.0288
  -4.000   0.0566   0.01177   0.00528  -0.0962   0.5972   0.0293
  -3.750   0.0835   0.01155   0.00501  -0.0960   0.5931   0.0297
  -3.500   0.1098   0.01130   0.00470  -0.0956   0.5887   0.0299
  -3.250   0.1361   0.01103   0.00439  -0.0952   0.5845   0.0301
  -3.000   0.1615   0.01046   0.00382  -0.0947   0.5811   0.0304
  -2.750   0.1874   0.01009   0.00343  -0.0943   0.5773   0.0307
  -2.500   0.2134   0.00981   0.00312  -0.0940   0.5736   0.0311
  -2.250   0.2396   0.00963   0.00289  -0.0936   0.5695   0.0316
  -2.000   0.2668   0.00942   0.00269  -0.0934   0.5664   0.0321
  -1.750   0.2942   0.00925   0.00251  -0.0932   0.5630   0.0326
  -1.500   0.3214   0.00912   0.00236  -0.0930   0.5592   0.0335
  -1.250   0.3484   0.00903   0.00223  -0.0928   0.5552   0.0345
  -1.000   0.3757   0.00895   0.00213  -0.0926   0.5515   0.0352
  -0.750   0.4035   0.00885   0.00204  -0.0925   0.5480   0.0358
  -0.500   0.4309   0.00874   0.00191  -0.0923   0.5440   0.0375
  -0.250   0.4581   0.00869   0.00183  -0.0921   0.5398   0.0396
   0.000   0.4853   0.00865   0.00178  -0.0919   0.5357   0.0433
   0.250   0.5113   0.00829   0.00172  -0.0916   0.5319   0.1416
   0.500   0.5342   0.00764   0.00171  -0.0910   0.5276   0.3633
   0.750   0.5581   0.00731   0.00176  -0.0904   0.5230   0.5070
   1.000   0.5837   0.00716   0.00181  -0.0899   0.5186   0.5851
   1.250   0.6097   0.00704   0.00185  -0.0895   0.5140   0.6423
   1.500   0.6347   0.00694   0.00189  -0.0889   0.5091   0.6986
   1.750   0.6576   0.00678   0.00195  -0.0878   0.5041   0.7767
   2.000   0.7333   0.00648   0.00207  -0.0981   0.4968   0.9848
   2.250   0.7779   0.00660   0.00213  -0.1019   0.4903   1.0000
   2.500   0.8032   0.00666   0.00217  -0.1013   0.4849   1.0000
   2.750   0.8280   0.00674   0.00221  -0.1007   0.4783   1.0000
   3.000   0.8526   0.00684   0.00228  -0.1000   0.4719   1.0000
   3.250   0.8777   0.00693   0.00234  -0.0994   0.4653   1.0000
   3.500   0.9018   0.00706   0.00241  -0.0987   0.4584   1.0000
   3.750   0.9271   0.00714   0.00249  -0.0982   0.4515   1.0000
   4.000   0.9510   0.00729   0.00258  -0.0974   0.4430   1.0000
   4.250   0.9758   0.00740   0.00267  -0.0968   0.4340   1.0000
   4.500   0.9997   0.00756   0.00279  -0.0961   0.4248   1.0000
   4.750   1.0233   0.00773   0.00290  -0.0953   0.4141   1.0000
   5.000   1.0477   0.00787   0.00302  -0.0947   0.4057   1.0000
   5.250   1.0710   0.00806   0.00317  -0.0938   0.3970   1.0000
   5.500   1.0954   0.00820   0.00330  -0.0932   0.3892   1.0000
   5.750   1.1186   0.00840   0.00346  -0.0924   0.3808   1.0000
   6.000   1.1426   0.00856   0.00362  -0.0917   0.3727   1.0000
   6.250   1.1655   0.00878   0.00379  -0.0909   0.3637   1.0000
   6.500   1.1879   0.00901   0.00398  -0.0900   0.3532   1.0000
   6.750   1.2113   0.00920   0.00416  -0.0892   0.3448   1.0000
   7.000   1.2331   0.00946   0.00438  -0.0882   0.3351   1.0000
   7.250   1.2556   0.00968   0.00458  -0.0874   0.3258   1.0000
   7.500   1.2777   0.00992   0.00480  -0.0864   0.3180   1.0000
   7.750   1.2988   0.01019   0.00504  -0.0853   0.3081   1.0000
   8.000   1.3205   0.01043   0.00527  -0.0844   0.2990   1.0000
   8.250   1.3405   0.01073   0.00554  -0.0831   0.2901   1.0000
   8.500   1.3616   0.01097   0.00578  -0.0820   0.2812   1.0000
   8.750   1.3808   0.01129   0.00607  -0.0806   0.2711   1.0000
   9.000   1.3974   0.01166   0.00639  -0.0788   0.2578   1.0000
   9.250   1.4110   0.01207   0.00674  -0.0764   0.2434   1.0000
   9.500   1.4227   0.01254   0.00715  -0.0737   0.2269   1.0000
   9.750   1.4286   0.01328   0.00774  -0.0701   0.2021   1.0000
  10.000   1.4292   0.01428   0.00856  -0.0660   0.1696   1.0000
  10.250   1.4179   0.01592   0.00991  -0.0605   0.1242   1.0000
  10.500   1.4058   0.01783   0.01159  -0.0556   0.0864   1.0000
  10.750   1.4086   0.01914   0.01285  -0.0529   0.0713   1.0000
  11.000   1.4060   0.02091   0.01449  -0.0501   0.0486   1.0000
  11.250   1.3973   0.02328   0.01673  -0.0471   0.0261   1.0000
  11.500   1.4016   0.02491   0.01837  -0.0455   0.0214   1.0000
  11.750   1.4076   0.02648   0.01997  -0.0442   0.0195   1.0000
  12.000   1.4137   0.02812   0.02166  -0.0430   0.0181   1.0000
  12.250   1.4215   0.02968   0.02328  -0.0421   0.0175   1.0000
  12.500   1.4266   0.03154   0.02520  -0.0412   0.0166   1.0000
  12.750   1.4298   0.03364   0.02736  -0.0404   0.0159   1.0000
  13.000   1.4303   0.03610   0.02990  -0.0397   0.0152   1.0000
  13.250   1.4332   0.03837   0.03225  -0.0391   0.0149   1.0000
  13.500   1.4376   0.04054   0.03449  -0.0387   0.0146   1.0000
  13.750   1.4399   0.04298   0.03700  -0.0383   0.0142   1.0000
  14.000   1.4419   0.04546   0.03954  -0.0380   0.0136   1.0000
  14.250   1.4422   0.04815   0.04230  -0.0377   0.0135   1.0000
  14.500   1.4414   0.05099   0.04521  -0.0374   0.0130   1.0000
  14.750   1.4378   0.05420   0.04849  -0.0372   0.0128   1.0000
  15.000   1.4318   0.05771   0.05209  -0.0371   0.0125   1.0000
  15.250   1.4174   0.06233   0.05681  -0.0371   0.0121   1.0000
  15.500   1.4160   0.06547   0.06003  -0.0372   0.0120   1.0000
  15.750   1.4148   0.06859   0.06323  -0.0373   0.0119   1.0000
  16.000   1.4102   0.07220   0.06692  -0.0375   0.0118   1.0000
  16.250   1.4085   0.07549   0.07029  -0.0378   0.0116   1.0000
  16.500   1.4038   0.07924   0.07412  -0.0382   0.0114   1.0000
  16.750   1.3996   0.08290   0.07786  -0.0386   0.0112   1.0000
  17.000   1.3950   0.08669   0.08172  -0.0391   0.0110   1.0000
  17.250   1.3907   0.09046   0.08557  -0.0397   0.0108   1.0000
  17.500   1.3853   0.09447   0.08965  -0.0404   0.0106   1.0000
  17.750   1.3794   0.09855   0.09381  -0.0412   0.0106   1.0000
  18.000   1.3744   0.10254   0.09786  -0.0420   0.0104   1.0000
  18.250   1.3697   0.10654   0.10192  -0.0430   0.0102   1.0000
  18.500   1.3626   0.11097   0.10643  -0.0441   0.0101   1.0000
  18.750   1.3552   0.11548   0.11099  -0.0454   0.0099   1.0000
  19.000   1.3484   0.11987   0.11545  -0.0467   0.0098   1.0000
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